Extra 200 - Page 130

CHAPTER 20
PAGE 13
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RA - FLUGZEUGBAU GmbH
SERVICE MANUAL EXTRA 200
PAGE DATE: 1. July 1996
5 Inspect all removed items for damage prior to assem-
bly. Damaged items have to be replaced or if possible
repaired according to Chapter 51.
C A U T I O N In order to prevent the aircraft from nosing over the
assembly has always to start with the empennage.
6 Prior to assembly remove engine cowlings, canopy,
main fuselage cover including the rear support angle
per Chapters 51 and 53.
N O T E In contrast to the instructions given in the respective
Chapters dont reinstall these items before completion
of the whole assembly.
7 Remove provisional attached rudder and vertical sta-
bilizer per Chapters 27 and 55.
8 Install horizontal stabilizer with elevator per Chapter
55. The procedure described there is also applicable to
the installation of the complete horizontal tail. Con-
sider to connect the ground bonding lead of the eleva-
tor too.
9 Connect elevator push pull rod actuator lever per Chap-
ter 27-01-01.
10 Connect trim wire to the tab actuator lever using fitted
clamp.
11 Inspect for full travel and elevator deflection in rela-
tion to stick movement.
12 Inspect for full travel and trim tab deflection in rela-
tion to trim handle movement.
13 Install the vertical stabilizer per Chapter 55.
14 Reinstall rudder to the vertical stabilizer per Chapter
27-21-01.
15 Inspect for full travel and rudder deflection in relation
to rudder pedal movement.
16 Install the wing per Chapter 57.
17 Install navigation/strobe lights per Chapter 33-41-01.
ASSEMBL
Y INSTRUCTION
Assembly Instruction after Container Shipping